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Relating NDT data to mechanical performance loss in Impact-damaged composites

机译:将NDT数据与冲击损坏复合材料中的机械性能损失联系起来

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There is currently no accepted method of incorporating non-destructive test data, gained from the inspection of impact-damaged composites directly into finite element models capable of predicting remaining mechanical performance. An improved ability to relate non-destructive testing data to performance is vital to allow damaged composites to be assessed rapidly and effectively prior to continued use, repair or replacement. This paper presents finite element simulations of the compression after impact tests performed on polymer-matrix composite laminates reinforced by unidirectional carbon fibres. These tests are performed on laboratory coupons, which are monolithic, flat, rectangular composite plates with conventional stacking sequences. The tests are simulated using conventional failure criteria for fibre, matrix damage and interlaminar delamination. Ultrasonic data acquired from the impact-damaged panels are incorporated automatically into the simulations to generate the initial condition of the laminates in terms of delaminations and matrix cracks. Good correspondence is achieved between simulation and experiment for aspects such as force-displacement responses, and buckling behaviour prior to final failure.
机译:目前没有采用非破坏性测试数据的接受方法,从冲击损坏的复合材料的检查中直接进入有限元模型,能够预测剩余的机械性能。改进的无损检测数据与性能相关的能力至关重要,允许在继续使用,修理或更换之前快速且有效地评估损坏的复合材料。本文介绍了通过单向碳纤维增强的聚合物 - 基质复合层压材料对冲击试验后的有限元模拟。这些测试是在实验室优惠券上进行的,该试样是具有常规堆叠序列的单片,平坦的矩形复合板。使用常规故障标准模拟测试,用于纤维,矩阵损伤和层间分层。从冲击损坏的面板获取的超声波数据被自动结合到模拟中以在分层和矩阵裂缝方面产生层压板的初始条件。在仿真和实验之间实现了良好的对应关系,例如在最终失败之前的力 - 位移应答和屈曲行为等方面。

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